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Easa Part 66 Module 11 B1 - Turbine Aeroplane Structures & Systems
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Overview
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Turbine Aeroplane Structures and Systems covers (by ATA chapter) the construction and operation of the various systems in complex turbine powered aircraft from their basic layout to their operation and maintenance needs from the perspective of the aircraft mechanic. Systems are covered by ATA chapters and include the general structures of transport category aircraft and various systems such as electrical, fuel, flight controls, hydraulics, etc) and also including modern on-board electronics such as on-board maintenance computers, cabin systems, and information systems. You will learn by understanding concepts, not just rote memorization and you will learn to understand and apply this knowledge in the MRO of flightline environment.
This book is fully compliant as EASA Part 66 module 11a for the B1 license and has been given approvals by numerous EASA based civil aviation authorities. |
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WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov. |
Table of Contents
11.1 Theory of Flight- airplane aerodynamics and flight controls; high speed flight.
- airworthiness requirements and structural strength; construction methods; structural assembly techniques; methods of surface protection; surface cleaning; airframe symmetry
- fuselage; wings; stabilizers; flight control surfaces; nacelles and pylons.
- air supply; air conditioning; pressurization; safety and warning devices.
- pitot static system, gyroscopic instruments; compasses; angle of attack indication; glass cockpit; avionics systems including autoflight, communications, navigation.
- Batteries; DC and AC power generation; emergency power generation; voltage regulation; power distribution; inverters, transformers, rectifiers; circuit protection; external ground power.
- emergency equipment requirements; cabin layout; cabin entertainment; galley installation; cargo handling; airstairs.
- fire and smoke detection; fire extinguishing systems; portable fire extinguisher.
- Primary controls - aileron, elevator, rudder, spoiler; trim control; active load control; high lift devices; lift dump and speed brakes; system operation - manual, hydraulic, pneumatic, electrical, fly-by-wire; artificial feel - yaw damper, Mach trim, rudder limiter, gust lock systems; balance and rigging; stall protection.
- system layout; fuel tanks; supply systems; dumping, venting, draining; cross feed and transfer; indications and warning; refueling and defueling; longitudinal balance.
- ice formation, classification and detection; anti-icing systems - electrical, hot air, and chemical; rain repellent; probe and drain heating; wiper systems.
- construction; shock absorbing; extension and retraction systems; indications and warning; wheels, brakes, antiskid, and autobraking; tires; steering; air-ground sensing.
- external navigation, anti-collision, landing, taxiing, ice; internal cabin, cockpit, cargo; emergency.
- system layout - cockpit and cabin; sources, storage, charging, and distribution; supply regulation; indication and warning.
- system layout, supply, distribution, servicing and draining; toilet system layout, flushing and servicing; corrosion aspects.
- system layout, supply, distribution, servicing and draining; toilet system layout, flushing and servicing; corrosion aspects.
- central maintenance computers, data loading system; electronic library system; printing; structure monitoring.
- integrated modular avionic (IMA) modules including bleed management, air pressure control, ventilation control, temperature control, air traffic communications, avionics communication router, electrical load management, electrical system BITE, fuel management, braking control, oleo pressure, gear retraction, etc; core system network components.
- cabin core systems; in-flight entertainment; external communications; cabin mass memory system; cabin monitoring systems; miscellaneous cabin systems.
- aircraft general information system; flight deck information system; maintenance information system; cabin information system; miscellaneous information systems.
Specifications
- Publisher: Aircraft Technical Book Co.
- ISBN-13: 9781941144947
- Copyright Date: 2020
- Edition: 4TH
- Pages: 680
- Binding: Paperback
- Dimensions: 11.0" x 8.5"
- Book Weight: 1.0lbs
- eBook
- File Type: standard pdf ebook
- Print: unlimited
- Copy/Paste: unlimited
- Offline Access: yes
- Search: always
- Bookmarks: always
- System Reqs: Windows, Macintosh, iPad, and more
Version Types
Softcover Book - Printed book with heavyweight cover stock.
eBook EB - A protected document designed for reflowable content. Also referred to as an ePub or "Electronic Publication" format. Easily viewed on both small and large screens. Text, images, and pages will adapt or reflow to fit the screen size of the device, so zooming is not necessary to read. Text size can be adjusted in an ebook reader app. Visit AC Technical Books -eBooks for more details on how to setup your device.
Q&A
Please note, Aircraft Spruce ®'s personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce ® assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
